# Service difficulty reports: N927UP, cancelled Aug 24, 2007

A list on [N927UP, cancelled Aug 24, 2007](https://openairdocs.org/deregistered/N927UP-2007-08-24.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 186 reports

- [SDR UPS04243402](https://openairdocs.org/sdr/UPS04243402.md): Bulb · inoperative · Oct 22, 2004 · N927UP · Boeing 72731C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH OFF IND BULB INOP. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH OFF IND BULB IAW 33-1000.
- [SDR UPS03241537](https://openairdocs.org/sdr/UPS03241537.md): Skin · cracked · Oct 19, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, NLG WW BS 259 SUSPECT CRACKS AT RIVETS AT RT AFT PRESSURE PANEL FWD EDGE. HFEC CONFIRMED CRACKS. AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC CONFIRMS DEFECT FREE CUTOUT. REPAIRED CUTOUT IAW SRM 51-40-2 FIG 1.
- [SDR UPS03241535](https://openairdocs.org/sdr/UPS03241535.md): Skin · cracked · Oct 19, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, NLG WW BS 263 AND BS 267 ROW OF RIVETS HAVE SUSPECT CRACKS ABOVE RT AFT PRESSURE PANEL. HFEC CONFIRMED CRACKS. AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC NDF REPAIRED CUTOUT IAW SRM 51-40-2 FIG 1.
- [SDR UPS03241534](https://openairdocs.org/sdr/UPS03241534.md): Pressure Panel · cracked · Oct 19, 2003 · N927UP · Boeing 72731C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C NLG W/W BS 290 LBL 0 SUSPECT CRACKS IN ROW OF RIVETS AT NLG CEILING. AREA CUTOUT IAW SRM 51-40-2 FIG 1, HFEC NDF. REPAIRED CUTOUT IAW SRM 51-10-2 FIG 1.
- [SDR UPS03241526](https://openairdocs.org/sdr/UPS03241526.md): Fitting · cracked · Oct 18, 2003 · N927UP · Boeing 72731C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C, TO REMOVE RT BS 930 FITTING, PARTIAL SHELF ATTACHING BS 930 TO 940 MUST BE REMOVED, ON REMOVAL OF PARTIAL SHELF AT STR 14 BS 930-940, 3 SUSPECT CRACKS WERE DETECTED ON MOST UPPER HORIZONTAL FLANGE (FWD SIDE) ON BS 940 FITTING. REPAIR CARR
- [SDR UPS03241533](https://openairdocs.org/sdr/UPS03241533.md): Skin · corroded · Oct 16, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AREA OF SURFACE CORROSION ON SKIN AT BS 1090 S12L. AREA REPAIRED IAW SMRO EO 2003-055-002 AND UPS FILE 727-53-20131.
- [SDR UPS03241532](https://openairdocs.org/sdr/UPS03241532.md): Support Bracket · cracked · Oct 15, 2003 · N927UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C RT WING I/B MID FLAP GUIDE ROLLER SUPPORT BRACKET CRACKED AT UPPER CHORD REAR SPAR JUST O/B OF NR 6 FLAP TRANSMISSION. ROLLER SUPPORT REPLACED IAW SRM 51-30-02 AND BOEING DRG 65-16201.
- [SDR UPS03241529](https://openairdocs.org/sdr/UPS03241529.md): Skin · cracked · Oct 14, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, SUSPECT CRACK AT NR 3 RT COCKPIT WINDOW CUTOUT AFT LWR CORNER. REPAIR CARRIED OUT IAW SRM 51-30-02, 53-30-03, 51-10-02 & 51-20-04.
- [SDR UPS03241527](https://openairdocs.org/sdr/UPS03241527.md): Fitting · cracked · Oct 11, 2003 · N927UP · Boeing 72731C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C, RT 930 FITTING HS SUSPECT CRACK AT AFT O/B FLANGE AT FLOOR LEVEL. REPAIR & REPLACEMENT OF BS 930 FITTING & ASSOCIATED STURCTURAL ITEMS CARRIED OUT IAW SMRO EO 2003-055-001 UPS ENGINEERING FILE 727-53-20 130.
- [SDR UPS03241518](https://openairdocs.org/sdr/UPS03241518.md): Skin · cracked · Oct 11, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, CABIN AIR PRESS LEAK FROM NR 1 VHF ANTENNA CUTOUT (AFT). ON INVESTIGATION A SUSPECT CRACK FOUND AT ANTENNA CUTOUT. HFEC INSPECTION CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM PT 6 51-00-00 FIG 4. CRACKEDCONFIRMED & MARKED. REPAIR CARRIE
- [SDR UPS03241538](https://openairdocs.org/sdr/UPS03241538.md): Fitting · cracked · Oct 10, 2003 · N927UP · Boeing 72731C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C SUSPECT CRACK ON ACTUATOR FITTING I/B LUG I/B FACE BELOW BOLT HOLE AIRSTAIRS ACTUATOR. HFEC CONFIRMED CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-30-02 AND DRAWING 65C13874. BOLT ALSO FOUND WORN, REPLACED IAW 52-62-71. OPS CHECKED SATI
- [SDR UPS03241536](https://openairdocs.org/sdr/UPS03241536.md): Skin · cracked · Oct 10, 2003 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, NLG WW BS 243 ROW OF RIVETS BELOW RT FWD PRESSURE PANEL HAVE CRACKS. HFEC CORFIRMED CRACKS, AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC COFIRMS NDF ON CUTOUT, REPAIRED IAW SRM 51-40-2 FIG 1.
- [SDR UPS03241517](https://openairdocs.org/sdr/UPS03241517.md): Panel · cracked · Oct 10, 2003 · N927UP · Boeing 72731C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, DURING PRESSURE LEAKAGE CHECK IN NLG WW A 3 INCH CRACK WAS FOUND ON RT CEILING. DAMAGED PART OF WEB CUTOUT REMOVED IAW SRM 51-40-2. DE-RIVETED IAW SRM 51-30-02. HFEC INSPECTION CARRIED OUT AROUND CUTOUT IN NWW ON RT CEILING IAW B727 NDT
- [SDR UPS03241528](https://openairdocs.org/sdr/UPS03241528.md): Fitting · damaged · Oct 3, 2003 · N927UP · Boeing 72731C · Nose/Tail Landing Gear
  > INSPECTION TYPE: C, REPLACED NLG DRAG BRACE FITTING AS PER EO B727-5340-0167.
- [SDR UPS02238550](https://openairdocs.org/sdr/UPS02238550.md): Beam · cracked · May 31, 2002 · N927UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK INDICATION AT BS 1183 BEAM RBL 26.83 WL 250 APPROX. REPAIR CARRIED OUT IAW EO B727-5311-0631 APPENDIX D
- [SDR UPS02238548](https://openairdocs.org/sdr/UPS02238548.md): Beam · cracked · May 30, 2002 · N927UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK INDICATING AT BS 1183 BEAM LBL 26.83 WL AT 250 APPROX REPAIR CARRIED OUT IAW EO B727-5311-0631 APPENDIX D
- [SDR UPS02238549](https://openairdocs.org/sdr/UPS02238549.md): Floorbeam · corroded · May 28, 2002 · N927UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C, CORROSION ON CHORD AT FLOOR LEVEL AT BS 1177 RT O/B. CHORD REPLACED IAW SRM 51-30-02 AND DRAWING 65-19606.
- [SDR UPS02238551](https://openairdocs.org/sdr/UPS02238551.md): Rib · cracked · May 27, 2002 · N927UP · Boeing 72731C · Leading Edge Slat Control System
  > INSPECTION TYPE:C RIB CRACKED ON LE SLAT #3, RIB LOCATED I/B OF O/B TRACK #3 SLAT REMOVED TO CARRY OUT REPAIR ON CRACKED RIB IAW MM 27-81-11 CRACKED RIB REPAIRED IAW SRM 57-50-3 FIG 9 #3 SLAT INSTALLED AFTER REPAIR COMPLETED IAW MM 27-81-11
- [SDR UPS02238547](https://openairdocs.org/sdr/UPS02238547.md): Skin · corroded · May 27, 2002 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SURFACE CORROSION ON FUSELAGE SKIN INTERNAL AT BS 254.5 BETWEEN STR 5L & 6L. REPAIR CARRIED OUT IAW DRAWING 692161 & UPS EO B727-5310-1371 APPENDIX E.
- [SDR UPS02238518](https://openairdocs.org/sdr/UPS02238518.md): Seat Track · corroded · May 27, 2002 · N927UP · Boeing 72731C · Cabin Equipment/Furnishings
  > INSPECTION TYPE:C CORROSION ON SEAT TRACK AT BS 660 AND BS 680 LBL 62.5 SEAT TRACK REPLACED BS 655 BS 710 LBL 62.5 IAW SRM 53-10-5 FIGURE 1
- [SDR UPS02238556](https://openairdocs.org/sdr/UPS02238556.md): Skin · cracked · May 23, 2002 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CRACK IN SECTION 41 FUSELAGE SKIN AT BS 211.8 R/H AT WL 197.5 REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3 USING 0.063" DOULER IAW EO B727-5330-0795-G
- [SDR UPS02238555](https://openairdocs.org/sdr/UPS02238555.md): Skin · corroded · May 22, 2002 · N927UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CORROSION BETWEEN SKIN & INTERNAL DOUBLER AT BS 1180 BETWEEN S10L & 9L. REPAIR CARRIED OUT IAW SRM 51-10-6 & 53-30-3, DAMAGE CUT OUT IAW 51- 10-6. REPAIRED IAW 51-10-2 AND 53-30-3 FIG 1 STEP 4.
- [SDR UPS02238554](https://openairdocs.org/sdr/UPS02238554.md): Door Frame · cracked · May 22, 2002 · N927UP · Boeing 72731C · Passenger/Crew Doors
  > INSPECTION TYPE:C ON REMOVAL OF AFT LWR STOP WHICH IS CRACKED, DOOR FRAME FOUND CRACKE D AT LWR END ON FWD ENTRY DOOR REPAIR CARRIED OUT IAW SMRO EO 2002-031-002 UPS ENGINEERING FILE NO 727-52-20009
- [SDR UPS02238553](https://openairdocs.org/sdr/UPS02238553.md): Door Frame · cracked · May 21, 2002 · N927UP · Boeing 72731C · Passenger/Crew Doors
  > INSPECTION TYPE:C CRACK IN DOOR FRAME AT AFT UPPER CORNER OF FWD ENTRY DOOR DOOR FRAME REPLACED IAW SMRO EO 2002-031-001 UPS ENGINEERING FILE NO. 727-52-20008
- [SDR UPS02238552](https://openairdocs.org/sdr/UPS02238552.md): Slat · cracked · May 21, 2002 · N927UP · Boeing 72731C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C DENTS ON SLAT POSITIONS 6 & 8 DENTS RE-WORKED IAW SRM 51-40-1 HFEC INSP. CARRIED OUT IAW NDT MANUAL, PART 6 51-00-00 FIG 4 - #8 S LAT NDF. #6 SLAT SKIN CRACKED & CRACK ENDS MARKED. #6 SLAT REPAIRED IAW SRM 57-30-03 SLAT REMOVED & INSTALL
- [SDR UPS02238545](https://openairdocs.org/sdr/UPS02238545.md): Stop Fitting · cracked · May 21, 2002 · N927UP · Boeing 72731C · Passenger/Crew Doors
  > INSPECTION TYPE:C 2 SUSPECT CRACKS ON LWR AFT ADJUSTABLE STOP FITTING ON FWD ENTRY DOO R STOP FITTING REPLACED IAW SMRO EO 2002-031-002 UPS ENGINEERING FILE NO. 727-52-20009
- [SDR UPS02238544](https://openairdocs.org/sdr/UPS02238544.md): Stop Fitting · cracked · May 21, 2002 · N927UP · Boeing 72731C · Passenger/Crew Doors
  > INSPECTION TYPE:C 2 SUSPECT CRACKS ON LWR AFT ADJUSTABLE STOP FITTING ON FWD ENTRY DOO R STOP FITTING REPLACED IAW SMRO EO 2002-031-002 UPS ENGINEERING FILE NO. 727-52-20009
- [SDR UPS01234750](https://openairdocs.org/sdr/UPS01234750.md): Bracket · cracked · Jan 9, 2001 · N927UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, ATTACH BRACKET LOCATED ON LT 870 FITTING IS CRACKED ALONG BEND LINE. BRACKET DERIVETED IAW SRM 51-30-02, BRACKET FABRICATED IAW SRM 51-20- 01, BRACKET INSTALLED IAW SRM 51-30-02.
- [SDR UPS01234748](https://openairdocs.org/sdr/UPS01234748.md): Bracket · cracked · Jan 9, 2001 · N927UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CK ATTACH BRACKET LOCATED ON LT BS 870 FITTING IS CRACKED ALONG BEND LINE. BRACKET DE-RIVETED. HEAT TREATMENT. BRACKET FABRICATED. BRACKET INSTALLED.
- [SDR UPS01234660](https://openairdocs.org/sdr/UPS01234660.md): Support Fitting · cracked · Jan 8, 2001 · N927UP · Boeing 72731C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, SUPPORT FITTING ON RT WING REAR SPAR AT WS 620 APPROX CRACKED. REPLACED SUPPORT FITTING WITH PART FABRICATED IAW DRAWING 69-16227.
- [SDR UPS01234659](https://openairdocs.org/sdr/UPS01234659.md): Support Fitting · cracked · Jan 8, 2001 · N927UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C, NR 7 FLAP TRACK ATTACH FITTING ON REAR SPAR CRACKED. FITTING REPLACED IAW SRM 51-30-02 AND DRAWING 65-16201.
- [SDR UPS01234749](https://openairdocs.org/sdr/UPS01234749.md): Skin Panel · corroded · Jan 7, 2001 · N927UP · Boeing 72731C · Elevator, Plate/Skin
  > INSPECTION TYPE:C CORROSION IN LT ELEVATOR UPPER SKIN UNDER STATIC DISCHARGER AT FS 238. SKIN REPLACED IAW DRAWING NR 65-25640.
- [SDR UPS01234747](https://openairdocs.org/sdr/UPS01234747.md): Panel · corroded · Jan 7, 2001 · N927UP · Boeing 72731C · Elevator, Plate/Skin
  > INSPECTION TYPE:CCK CORROSION IN LT ELEVATOR UPPER SKIN UNDER STATIC DISCHARGER. UPPER SKIN REPLACED IAW DRAWING NR 655640.
- [SDR UPS01234661](https://openairdocs.org/sdr/UPS01234661.md): Link · corroded · Jan 7, 2001 · N927UP · Boeing 72731C · Main Landing Gear Attach Section
  > INSPECTION TYPE:C, RT MAIN LANDING GEAR TRUNNION LINK CORRODED EXCESSIVELY AROUND SPLINED AREA, CHROME ALSO DAMAGED DUE TO CORROSION. RT TRUNNION LINK REPLACED IAW MM 32-11-01.
- [SDR UPS01234658](https://openairdocs.org/sdr/UPS01234658.md): Casting · corroded · Jan 5, 2001 · N927UP · Boeing 72731C · Spoilers
  > INSPECTION TYPE:C, NR 7 SPOILER INBOARD HINGE CASTING CORRODED. REPLACED NR 7 SPOILER INBOARD HINGE CASTING IAW SRM 51-30-02.
- [SDR UPS01234638](https://openairdocs.org/sdr/UPS01234638.md): Skin Panel · corroded · Jan 5, 2001 · N927UP · Boeing 72731C · Elevator, Plate/Skin
  > INSPECTION TYPE:C, CORROSION ON RT ELEVATOR UNDER STATIC DISCHARGER UPPER SKIN PANEL. SKIN PANEL REPLACED IAW BOEING DRAWING 65-25639.
- [SDR UPS01234635](https://openairdocs.org/sdr/UPS01234635.md): Fitting · cracked · Jan 5, 2001 · N927UP · Boeing 72731C · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:C NLG DRAG BRACE FITTING NDT COMFIRMED 2 CRACKS LOCATED ON THE SIDE OF INTERCOSTAL ATTACH FLANGE REF B727-5340-0166 FOR NDT CONFIRMATION. CARRIED OUT REPAIR AS PER EO B727-5340-0167MPI RAISED NR 12786.
- [SDR UPS01234636](https://openairdocs.org/sdr/UPS01234636.md): Fitting · corroded · Jan 3, 2001 · N927UP · Boeing 72731C · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:C, RT MLG UPLOCK ROLLER SUPPORT FITTING HAS EVIDENCE OF CORROSION BETWEEN SHIM AND FITTING AT UPPER ATTACH POINT. REPLACED FITTING IAW OHM 20-50-01.
- [SDR UPS99229993](https://openairdocs.org/sdr/UPS99229993.md): Floorbeam · corroded · Jun 18, 1999 · N927UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C&SI, DURING REPAIR OF FLOORBEAM 560 BETWEEN RBL 45.5 & 62.5 ADDITIONAL CORROSION FOUND AT FLANGE DURING INCORPERATION OF REPAIR ANGLES. FLOORBEAM BS 560 REPAIRED IAW SRMO EO 99-14-012 REV 1 UPS ENGINEERING FILE NR 727-53-2445.
- [SDR UPS99230004](https://openairdocs.org/sdr/UPS99230004.md): Fitting · cracked · Jun 15, 1999 · N927UP · Boeing 72731C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C&SI, CRACK INDICATION IN WING CENTER SECTION RT WING TERMINAL FITTING, LWR O/B FASTENER HOLE, BS 870. REPAIRED IAW SMRO EO 99416RI UPS EO NR B727-5710-11557-A.
- [SDR UPS99229989](https://openairdocs.org/sdr/UPS99229989.md): Spar Web · corroded · Jun 13, 1999 · N927UP · Boeing 72731C · Wing Spar
  > INSPECTION TYPE:C&SI, ON REMOVAL OF CENTER SECTION UPPER CHORD REAR SPAR BS 870, WEB FOUND CORRODED RBL 70.5 TO LBL 70.5. WEB REPLACED IAW SNN MRO EO 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.
- [SDR UPS99229987](https://openairdocs.org/sdr/UPS99229987.md): Spar Chord · corroded · Jun 13, 1999 · N927UP · Boeing 72731C · Wing Spar
  > INSPECTION TYPE:C&SI, ON REMOVAL OF CENTER SECTION WEB BS 870 RBL 70.5 TO LBL 70.5 LWR CHORD, REAR SPAR FOUND CORRODED. REPLACEMENT CHORD INSTALLED IAW SNN MRO EO NR 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.
- [SDR UPS99229848](https://openairdocs.org/sdr/UPS99229848.md): Web · cracked · Jun 10, 1999 · N927UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, BS 870 BBL 15 LT SIDE AIR CONDITIONING DOOR SUPPORT WEB STRUCTURE ATTACHED TO LWR END OF BS 870 BLKHD FOUND CRACKED. WEB REPAIRED IAW B727 SRM 51-40-2.
- [SDR UPS99229854](https://openairdocs.org/sdr/UPS99229854.md): Clevis · cracked · Jun 9, 1999 · N927UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C&SI SUPPORT STRUT ABOVE NR 2 ENGINE HORIZ FIREWALL LUG CRACKED AT LWR ATTACHMENT POINT. NR 2 ENGINE STRUCTURE SUPPORT STRUT LWR CLEVIS REPLACED PER SRM 51-30-2.
- [SDR UPS99229991](https://openairdocs.org/sdr/UPS99229991.md): Stiffener · corroded · Jun 7, 1999 · N927UP · Boeing 72731C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C&SI, ON REMOVAL OF FASTENERS CORROSION FOUND ON VERT STIFFENER BETWEEN UPPER & LWR WING CENTER SECTION SPAR CHORDS RBL 45. STIFFENER REPLACED IAW DRAWING 65-16202.
- [SDR UPS99229990](https://openairdocs.org/sdr/UPS99229990.md): Spar · corroded · Jun 7, 1999 · N927UP · Boeing 72731C · Wing Spar
  > INSPECTION TYPE:C&SI, ON REMOVAL OF FASTENERS CORROSION FOUND ON VERT FLANGE UPPER CHORD REAR SPAR BS 870 CENTER SECTION AT RBL 35 APPROX. UPPER CHORD REPLACED IAW SNN MRO EO 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.
- [SDR UPS99229849](https://openairdocs.org/sdr/UPS99229849.md): Splice · damaged · Jun 5, 1999 · N927UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, DAMAGE TO SPLICE PLATE AT STA 580 BETWEEN STR 25R AND STR 26R. REPLACED IAW SRM 53-10-2 FIG 3.
- [SDR UPS99229880](https://openairdocs.org/sdr/UPS99229880.md): Stringer · corroded · Jun 4, 1999 · N927UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C & SI, SURFACE CORROSION ON STRINGER 23R NESTING SECTION AT BS 448 APPROX. NESTING SECTION REPLACED IAW SRM 53-10-02 FIG AND SRM 53-10-3 FIG 1.
- [SDR UPS99229879](https://openairdocs.org/sdr/UPS99229879.md): Stringer · cracked · Jun 4, 1999 · N927UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C & SI, SUSPECT CRACK ON STRINGER 21R NESTING SECTION AT BS 448 APPROX. NESTING SECTION REPLACED IAW SRM 53-10-02.
- [SDR UPS99229878](https://openairdocs.org/sdr/UPS99229878.md): Angle · cracked · Jun 4, 1999 · N927UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C & SI, E & E BAY CRACK ON FLOOR SUPPORT ANGLES AT BS 380 OVER STRINGER 25R. REPAIRED IAW SRM 51-40-3 FIG 1 AND REPROTECTED IAW SRM 51-10-2.

Next page: https://openairdocs.org/deregistered/N927UP-2007-08-24/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N927UP' AND deregistration_id = 'N927UP-2007-08-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N927UP-2007-08-24/reports

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